View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00116U 26083.99704175 +.00000000 +00000-0 +61008-4 0 00001
2 00116 66.8074 96.8412 0079096 327.7192 31.9059 13.92315124 01
| Epoch (UTC): | 24 March 2026 23:55:44 |
| Eccentricity: | 0.0079096 |
| inclination: | 66.8074° |
| perigee height: | 863 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 96.8412° |
| argument of perigee: | 327.7192° |
| revolutions per day: | 13.92315124 |
| mean anomaly at epoch: | 31.9059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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